Eclipse EA500 - GPS 3 - Installation; General; Job Set-Up; Procedure

GPS 3 - INSTALLATION
AMM-34-50-11-041-C-801
1. General
A.
This task gives procedures to install the Global Positioning System (GPS 3) unit.
B. There is one GPS 3 installed on the aircraft under 131 CZ-B - Floor Panel, Aft Short, Left
Cabin.
2.
Job Set-Up
SUBTASK AMM-34-50-11-041-C-921-001
A.
Make sure aircraft is in same configuration as it was when removal task was completed.
Refer to AMM-34-50-11-001-C-801 – GPS 3- Removal .
B. Complete GPS 3 configuration (if not previously accomplished), refer to
AMM-34-50-10-051-B-801 – GPS 3- Maintenance Practices .
C. Make sure that mount backplate has the 50 ohm/5 watt termination load is installed on
coax receptacle BTM.
3.
Procedure
SUBTASK AMM-34-50-11-041-C-411-001
(Refer to Fig. 401.)
A.
Slide the GPS 3 unit (1) straight into the rack until it stops.
B. Lift the lock down arm (2) over the right angled hook on the unit and hand tightened.
C. Secure 131 CZ-B - Floor Panel, Aft Short, Left Cabin with four screws. Refer to
AMM-25-11-30-041-801 – Cockpit Floor Panels - Installation .
4.
Job Close-Up
SUBTASK AMM-34-50-11-041-C-921-002
A.
Remove all tools, equipment, and unwanted material from work area.
B. Do a system test of the ADS-B. Refer to SUBTASK AMM-34-50-20-071-C-701-005.
C. If all other maintenance is complete, return aircraft to service. Refer to
AMM-20-00-02-051-801 – Return To Service (After Maintenance).
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-34-030
34-50-11
CONFIG C
Page 401-Inst
Sep 30/20
© 2020 Eclipse Aerospace, Inc.